View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 82U 61004B 25142.84345537 .00000365 00000-0 33754-3 0 9993
2 82 38.8568 9.4251 1166761 136.7441 233.1053 12.27636259 28836
| Epoch (UTC): | 22 May 2025 20:14:34 |
| Eccentricity: | 0.1166761 |
| inclination: | 38.8568° |
| perigee height: | 633 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 9.4251° |
| argument of perigee: | 136.7441° |
| revolutions per day: | 12.27636259 |
| mean anomaly at epoch: | 233.1053° |
| orbit number at epoch: | 2883 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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